501 lines
89 KiB
Plaintext
501 lines
89 KiB
Plaintext
18.1x12 (181x12.dat)
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v2022-0915
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Simulation Date: 09/22/2022
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AIRFOIL AERO DATA GENERATED USING: POLAR DIAGRAMS
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====== PERFORMANCE DATA (versus advance ratio and MPH) ======
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DEFINITIONS:
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J=V/nD (advance ratio)
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Ct=T/(rho * n**2 * D**4) (thrust coef.)
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Cp=P/(rho * n**3 * D**5) (power coef.)
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Pe=Ct*J/Cp (efficiency)
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V (model speed in MPH)
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Mach (at prop tip)
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Reyn (at 75% of span)
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FOM (Figure of Merit)
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PROP RPM = 1000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1078 0.0475 0.007 0.468 0.369 5.533 0.053 1.639 30.215 0.07 37985. 0.5947
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0.48 0.0282 0.0622 0.1065 0.0482 0.008 0.475 0.364 5.624 0.054 1.621 29.385 0.07 38015. 0.5750
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0.97 0.0564 0.1209 0.1051 0.0490 0.008 0.483 0.360 5.713 0.055 1.600 28.554 0.07 38049. 0.5551
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1.45 0.0846 0.1762 0.1036 0.0497 0.008 0.490 0.354 5.798 0.055 1.577 27.727 0.07 38085. 0.5351
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1.93 0.1127 0.2279 0.1020 0.0504 0.008 0.497 0.349 5.878 0.056 1.551 26.906 0.07 38125. 0.5151
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2.42 0.1409 0.2763 0.1001 0.0510 0.008 0.503 0.342 5.951 0.057 1.523 26.095 0.07 38169. 0.4950
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2.90 0.1691 0.3214 0.0981 0.0516 0.008 0.508 0.335 6.014 0.057 1.492 25.294 0.07 38217. 0.4749
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3.38 0.1973 0.3633 0.0958 0.0520 0.008 0.513 0.328 6.066 0.058 1.458 24.505 0.07 38268. 0.4548
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3.86 0.2255 0.4020 0.0934 0.0524 0.008 0.516 0.319 6.104 0.058 1.420 23.729 0.07 38324. 0.4347
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4.35 0.2537 0.4377 0.0907 0.0525 0.008 0.518 0.310 6.126 0.058 1.380 22.966 0.07 38383. 0.4146
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4.83 0.2818 0.4705 0.0877 0.0526 0.008 0.518 0.300 6.127 0.059 1.335 22.216 0.07 38447. 0.3946
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5.31 0.3100 0.5004 0.0846 0.0524 0.008 0.516 0.289 6.107 0.058 1.286 21.479 0.07 38514. 0.3745
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5.80 0.3382 0.5274 0.0811 0.0520 0.008 0.512 0.277 6.062 0.058 1.234 20.754 0.07 38586. 0.3543
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6.28 0.3664 0.5517 0.0774 0.0514 0.008 0.506 0.265 5.991 0.057 1.177 20.038 0.07 38662. 0.3342
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6.76 0.3946 0.5731 0.0734 0.0506 0.008 0.498 0.251 5.894 0.056 1.117 19.329 0.07 38743. 0.3141
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7.25 0.4228 0.5917 0.0693 0.0495 0.008 0.488 0.237 5.772 0.055 1.054 18.624 0.07 38828. 0.2939
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7.73 0.4510 0.6072 0.0650 0.0483 0.008 0.475 0.222 5.625 0.054 0.988 17.918 0.07 38917. 0.2738
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8.21 0.4791 0.6195 0.0605 0.0468 0.007 0.461 0.207 5.454 0.052 0.920 17.206 0.07 39010. 0.2537
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8.70 0.5073 0.6283 0.0559 0.0451 0.007 0.444 0.191 5.259 0.050 0.850 16.481 0.07 39107. 0.2336
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9.18 0.5355 0.6332 0.0511 0.0432 0.007 0.426 0.175 5.040 0.048 0.778 15.735 0.07 39209. 0.2133
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9.66 0.5637 0.6336 0.0463 0.0412 0.006 0.406 0.158 4.798 0.046 0.704 14.959 0.07 39315. 0.1929
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10.14 0.5919 0.6289 0.0413 0.0389 0.006 0.383 0.141 4.532 0.043 0.628 14.140 0.07 39425. 0.1723
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10.63 0.6201 0.6178 0.0363 0.0364 0.006 0.359 0.124 4.243 0.041 0.552 13.259 0.07 39540. 0.1514
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11.11 0.6482 0.5988 0.0312 0.0337 0.005 0.332 0.107 3.932 0.038 0.474 12.293 0.07 39658. 0.1301
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11.59 0.6764 0.5695 0.0260 0.0309 0.005 0.304 0.089 3.599 0.034 0.395 11.205 0.07 39781. 0.1083
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12.08 0.7046 0.5264 0.0208 0.0278 0.004 0.274 0.071 3.244 0.031 0.316 9.941 0.07 39908. 0.0859
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12.56 0.7328 0.4634 0.0156 0.0246 0.004 0.242 0.053 2.869 0.027 0.237 8.416 0.07 40040. 0.0630
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13.04 0.7610 0.3708 0.0103 0.0212 0.003 0.209 0.035 2.475 0.024 0.157 6.485 0.07 40175. 0.0395
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13.53 0.7892 0.2298 0.0052 0.0177 0.003 0.174 0.018 2.064 0.020 0.078 3.876 0.07 40315. 0.0167
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14.01 0.8174 0.0005 0.0000 0.0140 0.002 0.138 0.000 1.637 0.016 0.000 0.008 0.07 40456. 0.0000
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PROP RPM = 2000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1082 0.0432 0.054 1.701 1.481 40.246 0.192 6.586 16.687 0.14 75969. 0.6583
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0.97 0.0284 0.0690 0.1070 0.0440 0.055 1.734 1.464 41.023 0.196 6.512 16.186 0.14 76030. 0.6349
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1.94 0.0567 0.1337 0.1056 0.0448 0.056 1.766 1.445 41.787 0.200 6.429 15.688 0.14 76097. 0.6114
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2.92 0.0851 0.1943 0.1041 0.0456 0.057 1.797 1.425 42.524 0.203 6.337 15.195 0.14 76171. 0.5880
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3.89 0.1134 0.2508 0.1025 0.0463 0.058 1.827 1.402 43.219 0.206 6.235 14.710 0.14 76252. 0.5646
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4.86 0.1418 0.3033 0.1006 0.0470 0.059 1.853 1.376 43.858 0.209 6.122 14.234 0.14 76340. 0.5414
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5.83 0.1702 0.3521 0.0986 0.0476 0.060 1.877 1.348 44.422 0.212 5.998 13.768 0.14 76436. 0.5183
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6.81 0.1985 0.3972 0.0963 0.0481 0.060 1.897 1.318 44.894 0.214 5.861 13.313 0.14 76540. 0.4954
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7.78 0.2269 0.4388 0.0938 0.0485 0.061 1.912 1.284 45.253 0.216 5.711 12.869 0.14 76652. 0.4727
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8.75 0.2552 0.4771 0.0911 0.0488 0.061 1.922 1.247 45.478 0.217 5.547 12.437 0.14 76772. 0.4502
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9.72 0.2836 0.5121 0.0882 0.0488 0.061 1.925 1.207 45.542 0.217 5.367 12.016 0.14 76900. 0.4279
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10.69 0.3120 0.5442 0.0850 0.0487 0.061 1.920 1.162 45.422 0.217 5.170 11.607 0.14 77037. 0.4057
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11.67 0.3403 0.5733 0.0815 0.0484 0.060 1.906 1.115 45.100 0.215 4.958 11.209 0.14 77183. 0.3836
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12.64 0.3687 0.5996 0.0777 0.0478 0.060 1.883 1.063 44.565 0.213 4.729 10.821 0.14 77337. 0.3617
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13.61 0.3970 0.6231 0.0737 0.0470 0.059 1.852 1.009 43.817 0.209 4.487 10.442 0.14 77500. 0.3400
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14.58 0.4254 0.6438 0.0695 0.0460 0.057 1.811 0.952 42.856 0.205 4.232 10.070 0.14 77671. 0.3184
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15.56 0.4538 0.6617 0.0652 0.0447 0.056 1.762 0.892 41.687 0.199 3.967 9.703 0.15 77851. 0.2970
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16.53 0.4821 0.6766 0.0607 0.0432 0.054 1.704 0.830 40.310 0.192 3.691 9.338 0.15 78039. 0.2758
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17.50 0.5105 0.6883 0.0560 0.0415 0.052 1.637 0.766 38.730 0.185 3.407 8.971 0.15 78236. 0.2546
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18.47 0.5388 0.6964 0.0512 0.0396 0.050 1.561 0.701 36.948 0.176 3.116 8.600 0.15 78442. 0.2334
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19.44 0.5672 0.7006 0.0463 0.0375 0.047 1.478 0.634 34.964 0.167 2.818 8.219 0.15 78656. 0.2121
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20.42 0.5956 0.7001 0.0413 0.0351 0.044 1.385 0.565 32.780 0.157 2.515 7.822 0.15 78879. 0.1907
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21.39 0.6239 0.6939 0.0363 0.0326 0.041 1.285 0.496 30.399 0.145 2.206 7.400 0.15 79111. 0.1689
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22.36 0.6523 0.6803 0.0311 0.0298 0.037 1.176 0.426 27.823 0.133 1.893 6.940 0.15 79351. 0.1468
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23.33 0.6806 0.6568 0.0259 0.0269 0.034 1.059 0.355 25.057 0.120 1.578 6.421 0.15 79600. 0.1240
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24.30 0.7090 0.6193 0.0207 0.0237 0.030 0.934 0.283 22.107 0.106 1.260 5.812 0.15 79857. 0.1003
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25.28 0.7374 0.5604 0.0155 0.0204 0.025 0.802 0.212 18.983 0.091 0.941 5.057 0.15 80123. 0.0754
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26.25 0.7657 0.4662 0.0102 0.0168 0.021 0.663 0.140 15.699 0.075 0.624 4.051 0.15 80397. 0.0492
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27.22 0.7941 0.3057 0.0051 0.0132 0.016 0.519 0.069 12.270 0.059 0.308 2.562 0.15 80679. 0.0219
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28.19 0.8224 -0.0078 -0.0001 0.0093 0.012 0.367 -0.001 8.691 0.041 -0.005 -0.063 0.15 80958. 0.0000
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PROP RPM = 3000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1086 0.0415 0.175 3.679 3.344 130.564 0.416 14.875 11.618 0.22 113951. 0.6887
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1.46 0.0284 0.0721 0.1074 0.0423 0.179 3.755 3.307 133.269 0.424 14.709 11.255 0.22 114042. 0.6635
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2.92 0.0568 0.1396 0.1061 0.0432 0.182 3.830 3.265 135.934 0.433 14.525 10.896 0.22 114143. 0.6383
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4.38 0.0853 0.2026 0.1046 0.0440 0.186 3.902 3.219 138.512 0.441 14.319 10.541 0.22 114254. 0.6131
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5.85 0.1137 0.2613 0.1029 0.0448 0.189 3.971 3.168 140.953 0.449 14.091 10.194 0.22 114376. 0.5882
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7.31 0.1421 0.3157 0.1011 0.0455 0.192 4.035 3.111 143.201 0.456 13.838 9.854 0.22 114509. 0.5634
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8.77 0.1705 0.3661 0.0990 0.0461 0.195 4.091 3.048 145.199 0.462 13.559 9.522 0.22 114654. 0.5390
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10.23 0.1990 0.4126 0.0968 0.0467 0.197 4.138 2.979 146.882 0.468 13.251 9.200 0.22 114810. 0.5148
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11.69 0.2274 0.4555 0.0943 0.0471 0.199 4.175 2.903 148.183 0.472 12.914 8.886 0.22 114979. 0.4909
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13.15 0.2558 0.4949 0.0916 0.0473 0.200 4.199 2.820 149.023 0.474 12.543 8.583 0.22 115160. 0.4672
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14.62 0.2842 0.5311 0.0886 0.0474 0.200 4.207 2.729 149.317 0.475 12.137 8.288 0.22 115353. 0.4438
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16.08 0.3127 0.5641 0.0854 0.0473 0.200 4.197 2.629 148.980 0.474 11.693 8.003 0.22 115560. 0.4207
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17.54 0.3411 0.5942 0.0819 0.0470 0.198 4.168 2.521 147.947 0.471 11.212 7.728 0.22 115779. 0.3977
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19.00 0.3695 0.6215 0.0781 0.0464 0.196 4.119 2.405 146.187 0.465 10.696 7.461 0.22 116011. 0.3750
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20.46 0.3979 0.6460 0.0741 0.0457 0.193 4.048 2.281 143.689 0.457 10.147 7.201 0.22 116256. 0.3526
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21.92 0.4264 0.6678 0.0699 0.0446 0.188 3.957 2.152 140.459 0.447 9.571 6.948 0.22 116514. 0.3304
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23.39 0.4548 0.6869 0.0655 0.0434 0.183 3.846 2.017 136.504 0.435 8.969 6.700 0.22 116785. 0.3085
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24.85 0.4832 0.7032 0.0610 0.0419 0.177 3.714 1.876 131.835 0.420 8.346 6.456 0.22 117069. 0.2867
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26.31 0.5116 0.7165 0.0563 0.0402 0.170 3.563 1.732 126.456 0.403 7.704 6.212 0.22 117366. 0.2650
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27.77 0.5401 0.7265 0.0515 0.0382 0.161 3.391 1.584 120.372 0.383 7.045 5.968 0.22 117676. 0.2435
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29.23 0.5685 0.7329 0.0465 0.0361 0.152 3.200 1.432 113.589 0.362 6.371 5.719 0.22 117999. 0.2219
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30.69 0.5969 0.7350 0.0415 0.0337 0.142 2.990 1.278 106.109 0.338 5.684 5.462 0.22 118335. 0.2002
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32.16 0.6253 0.7318 0.0364 0.0311 0.131 2.759 1.121 97.941 0.312 4.986 5.191 0.22 118684. 0.1782
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33.62 0.6538 0.7218 0.0313 0.0283 0.119 2.510 0.962 89.094 0.284 4.279 4.898 0.22 119046. 0.1557
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35.08 0.6822 0.7025 0.0260 0.0253 0.107 2.242 0.802 79.583 0.253 3.565 4.568 0.22 119420. 0.1326
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36.54 0.7106 0.6699 0.0208 0.0221 0.093 1.956 0.640 69.433 0.221 2.847 4.182 0.22 119808. 0.1085
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38.00 0.7390 0.6161 0.0155 0.0186 0.079 1.653 0.478 58.678 0.187 2.128 3.698 0.22 120208. 0.0829
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39.46 0.7675 0.5254 0.0103 0.0150 0.064 1.334 0.317 47.365 0.151 1.411 3.037 0.22 120621. 0.0554
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40.92 0.7959 0.3596 0.0051 0.0113 0.048 1.002 0.157 35.550 0.113 0.699 2.004 0.22 121045. 0.0258
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42.39 0.8243 -0.0086 -0.0001 0.0074 0.031 0.653 -0.002 23.179 0.074 -0.010 -0.046 0.22 121460. 0.0000
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PROP RPM = 4000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1091 0.0407 0.407 6.411 5.972 303.377 0.724 26.562 8.928 0.29 151929. 0.7073
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1.95 0.0285 0.0740 0.1079 0.0415 0.416 6.549 5.906 309.944 0.740 26.271 8.643 0.29 152051. 0.6810
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3.90 0.0569 0.1431 0.1066 0.0424 0.424 6.686 5.833 316.425 0.755 25.946 8.361 0.29 152186. 0.6547
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5.86 0.0854 0.2075 0.1051 0.0433 0.433 6.819 5.752 322.702 0.770 25.584 8.084 0.29 152335. 0.6285
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7.81 0.1139 0.2674 0.1034 0.0441 0.441 6.945 5.661 328.655 0.785 25.180 7.813 0.29 152498. 0.6026
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9.76 0.1423 0.3229 0.1016 0.0448 0.448 7.061 5.561 334.151 0.798 24.733 7.548 0.29 152676. 0.5770
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11.71 0.1708 0.3742 0.0996 0.0454 0.455 7.164 5.449 339.048 0.809 24.238 7.290 0.29 152869. 0.5517
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13.66 0.1993 0.4216 0.0973 0.0460 0.460 7.252 5.327 343.192 0.819 23.693 7.040 0.29 153078. 0.5267
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15.61 0.2277 0.4653 0.0949 0.0464 0.465 7.320 5.192 346.419 0.827 23.092 6.797 0.29 153303. 0.5021
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17.57 0.2562 0.5054 0.0922 0.0467 0.467 7.365 5.043 348.540 0.832 22.432 6.563 0.29 153546. 0.4778
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19.52 0.2847 0.5421 0.0892 0.0468 0.468 7.382 4.880 349.350 0.834 21.708 6.336 0.29 153805. 0.4538
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21.47 0.3131 0.5758 0.0859 0.0467 0.468 7.367 4.702 348.643 0.832 20.916 6.118 0.29 154081. 0.4301
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23.42 0.3416 0.6065 0.0824 0.0464 0.464 7.317 4.509 346.264 0.827 20.057 5.907 0.29 154374. 0.4066
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25.37 0.3701 0.6344 0.0786 0.0459 0.459 7.229 4.302 342.128 0.817 19.135 5.703 0.29 154685. 0.3835
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27.32 0.3985 0.6596 0.0746 0.0451 0.451 7.104 4.081 336.214 0.803 18.154 5.506 0.29 155013. 0.3606
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29.28 0.4270 0.6821 0.0703 0.0440 0.441 6.942 3.850 328.531 0.784 17.123 5.315 0.29 155358. 0.3381
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31.23 0.4555 0.7020 0.0659 0.0428 0.428 6.743 3.608 319.096 0.762 16.047 5.128 0.29 155720. 0.3158
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33.18 0.4839 0.7193 0.0613 0.0413 0.413 6.507 3.357 307.930 0.735 14.932 4.945 0.29 156100. 0.2937
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35.13 0.5124 0.7336 0.0566 0.0395 0.396 6.235 3.099 295.046 0.704 13.783 4.763 0.29 156498. 0.2718
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37.08 0.5409 0.7449 0.0518 0.0376 0.376 5.926 2.833 280.456 0.670 12.603 4.582 0.29 156912. 0.2500
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39.03 0.5693 0.7528 0.0468 0.0354 0.354 5.582 2.562 264.169 0.631 11.396 4.399 0.29 157344. 0.2283
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40.99 0.5978 0.7566 0.0418 0.0330 0.330 5.202 2.286 246.195 0.588 10.167 4.211 0.29 157793. 0.2064
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42.94 0.6263 0.7556 0.0366 0.0304 0.304 4.787 2.005 226.550 0.541 8.918 4.014 0.29 158260. 0.1842
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44.89 0.6547 0.7481 0.0314 0.0275 0.275 4.337 1.720 205.259 0.490 7.652 3.802 0.29 158744. 0.1617
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46.84 0.6832 0.7320 0.0262 0.0244 0.245 3.853 1.433 182.361 0.435 6.375 3.565 0.29 159245. 0.1384
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48.79 0.7117 0.7031 0.0209 0.0212 0.212 3.337 1.144 157.912 0.377 5.090 3.287 0.29 159763. 0.1140
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50.74 0.7401 0.6536 0.0156 0.0177 0.177 2.789 0.855 131.997 0.315 3.803 2.938 0.30 160299. 0.0881
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52.70 0.7686 0.5669 0.0104 0.0140 0.140 2.213 0.567 104.733 0.250 2.520 2.454 0.30 160851. 0.0599
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54.65 0.7971 0.3996 0.0051 0.0102 0.102 1.611 0.280 76.255 0.182 1.247 1.668 0.30 161417. 0.0286
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56.60 0.8255 -0.0133 -0.0001 0.0062 0.062 0.979 -0.005 46.343 0.111 -0.024 -0.054 0.30 161962. 0.0000
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PROP RPM = 5000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1097 0.0403 0.787 9.921 9.381 586.870 1.121 41.725 7.250 0.36 189903. 0.7198
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2.44 0.0285 0.0751 0.1085 0.0412 0.805 10.142 9.280 599.983 1.146 41.279 7.016 0.36 190055. 0.6928
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4.88 0.0569 0.1452 0.1072 0.0421 0.822 10.361 9.168 612.938 1.171 40.778 6.784 0.36 190224. 0.6659
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7.32 0.0854 0.2104 0.1057 0.0429 0.839 10.574 9.042 625.502 1.195 40.219 6.557 0.36 190410. 0.6391
|
|
9.76 0.1139 0.2711 0.1041 0.0437 0.855 10.775 8.902 637.430 1.217 39.595 6.334 0.36 190614. 0.6127
|
|
12.20 0.1424 0.3272 0.1023 0.0445 0.870 10.962 8.746 648.463 1.238 38.902 6.117 0.36 190836. 0.5865
|
|
14.64 0.1708 0.3791 0.1003 0.0452 0.883 11.128 8.573 658.314 1.257 38.134 5.907 0.36 191078. 0.5607
|
|
17.08 0.1993 0.4271 0.0980 0.0458 0.894 11.270 8.382 666.681 1.273 37.284 5.703 0.36 191340. 0.5352
|
|
19.52 0.2278 0.4712 0.0956 0.0462 0.903 11.381 8.172 673.232 1.286 36.348 5.505 0.36 191623. 0.5102
|
|
21.96 0.2563 0.5117 0.0929 0.0465 0.909 11.454 7.940 677.600 1.294 35.317 5.315 0.36 191926. 0.4855
|
|
24.40 0.2847 0.5489 0.0899 0.0466 0.911 11.485 7.686 679.377 1.298 34.186 5.131 0.36 192250. 0.4611
|
|
26.84 0.3132 0.5830 0.0866 0.0465 0.909 11.464 7.407 678.156 1.295 32.947 4.954 0.36 192596. 0.4371
|
|
29.28 0.3417 0.6141 0.0831 0.0462 0.903 11.387 7.104 673.621 1.287 31.600 4.784 0.36 192963. 0.4133
|
|
31.72 0.3702 0.6424 0.0793 0.0457 0.893 11.252 6.779 665.602 1.271 30.153 4.620 0.36 193352. 0.3899
|
|
34.16 0.3986 0.6682 0.0752 0.0449 0.877 11.056 6.433 654.051 1.249 28.614 4.461 0.36 193763. 0.3668
|
|
36.60 0.4271 0.6913 0.0710 0.0439 0.857 10.802 6.069 638.982 1.220 26.994 4.308 0.36 194195. 0.3440
|
|
39.04 0.4556 0.7118 0.0665 0.0426 0.832 10.488 5.689 620.434 1.185 25.303 4.159 0.36 194649. 0.3215
|
|
41.48 0.4841 0.7298 0.0619 0.0411 0.803 10.116 5.294 598.441 1.143 23.549 4.013 0.36 195125. 0.2993
|
|
43.92 0.5125 0.7450 0.0572 0.0393 0.768 9.687 4.888 573.035 1.094 21.741 3.869 0.36 195622. 0.2773
|
|
46.36 0.5410 0.7573 0.0523 0.0373 0.730 9.200 4.470 544.235 1.039 19.885 3.726 0.36 196141. 0.2554
|
|
48.80 0.5695 0.7663 0.0473 0.0351 0.687 8.656 4.044 512.061 0.978 17.986 3.582 0.36 196681. 0.2335
|
|
51.24 0.5980 0.7716 0.0422 0.0327 0.639 8.056 3.609 476.533 0.910 16.051 3.435 0.37 197243. 0.2115
|
|
53.69 0.6264 0.7723 0.0370 0.0300 0.587 7.399 3.167 437.682 0.836 14.085 3.282 0.37 197827. 0.1893
|
|
56.13 0.6549 0.7671 0.0318 0.0271 0.530 6.687 2.719 395.556 0.755 12.093 3.118 0.37 198432. 0.1666
|
|
58.57 0.6834 0.7537 0.0265 0.0240 0.470 5.920 2.267 350.232 0.669 10.082 2.936 0.37 199059. 0.1433
|
|
61.01 0.7118 0.7282 0.0212 0.0207 0.405 5.102 1.812 301.823 0.576 8.059 2.723 0.37 199708. 0.1188
|
|
63.45 0.7403 0.6830 0.0159 0.0172 0.336 4.235 1.356 250.498 0.478 6.032 2.456 0.37 200377. 0.0927
|
|
65.89 0.7688 0.6014 0.0105 0.0135 0.263 3.322 0.902 196.487 0.375 4.012 2.082 0.37 201068. 0.0641
|
|
68.33 0.7973 0.4377 0.0053 0.0096 0.188 2.368 0.451 140.062 0.267 2.007 1.461 0.37 201777. 0.0318
|
|
70.77 0.8257 0.0013 0.0000 0.0055 0.108 1.365 0.001 80.764 0.154 0.003 0.004 0.37 202456. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 6000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1104 0.0402 1.356 14.245 13.594 1011.238 1.609 60.466 6.097 0.43 227870. 0.7288
|
|
2.93 0.0285 0.0758 0.1093 0.0411 1.387 14.573 13.453 1034.476 1.646 59.838 5.898 0.43 228054. 0.7013
|
|
5.87 0.0570 0.1466 0.1080 0.0420 1.418 14.896 13.294 1057.459 1.683 59.130 5.702 0.43 228256. 0.6740
|
|
8.80 0.0856 0.2125 0.1065 0.0429 1.448 15.211 13.115 1079.771 1.719 58.337 5.509 0.43 228480. 0.6468
|
|
11.73 0.1141 0.2737 0.1049 0.0437 1.476 15.510 12.916 1100.978 1.752 57.450 5.321 0.43 228726. 0.6199
|
|
14.67 0.1426 0.3303 0.1031 0.0445 1.503 15.786 12.693 1120.608 1.784 56.460 5.138 0.43 228994. 0.5934
|
|
17.60 0.1711 0.3827 0.1011 0.0452 1.526 16.033 12.446 1138.161 1.811 55.359 4.960 0.43 229285. 0.5672
|
|
20.53 0.1996 0.4309 0.0988 0.0458 1.546 16.244 12.172 1153.094 1.835 54.139 4.788 0.43 229601. 0.5415
|
|
23.47 0.2282 0.4754 0.0964 0.0463 1.562 16.409 11.869 1164.827 1.854 52.792 4.622 0.43 229941. 0.5161
|
|
26.40 0.2567 0.5163 0.0937 0.0466 1.573 16.520 11.535 1172.708 1.866 51.306 4.461 0.43 230306. 0.4912
|
|
29.33 0.2852 0.5538 0.0907 0.0467 1.577 16.567 11.167 1176.024 1.872 49.671 4.307 0.43 230697. 0.4666
|
|
32.26 0.3137 0.5882 0.0874 0.0466 1.574 16.539 10.764 1174.055 1.869 47.878 4.158 0.43 231114. 0.4423
|
|
35.20 0.3423 0.6196 0.0839 0.0463 1.564 16.429 10.325 1166.239 1.856 45.927 4.016 0.43 231557. 0.4183
|
|
38.13 0.3708 0.6484 0.0800 0.0458 1.545 16.232 9.853 1152.270 1.834 43.828 3.879 0.43 232026. 0.3947
|
|
41.06 0.3993 0.6745 0.0759 0.0450 1.518 15.947 9.351 1132.058 1.802 41.593 3.746 0.43 232520. 0.3714
|
|
44.00 0.4278 0.6980 0.0716 0.0439 1.483 15.575 8.821 1105.634 1.760 39.238 3.619 0.43 233041. 0.3484
|
|
46.93 0.4563 0.7191 0.0672 0.0426 1.439 15.116 8.269 1073.062 1.708 36.779 3.495 0.44 233588. 0.3258
|
|
49.86 0.4849 0.7376 0.0625 0.0411 1.387 14.572 7.695 1034.411 1.646 34.227 3.374 0.44 234161. 0.3034
|
|
52.80 0.5134 0.7535 0.0577 0.0393 1.327 13.942 7.103 989.734 1.575 31.596 3.255 0.44 234760. 0.2813
|
|
55.73 0.5419 0.7665 0.0528 0.0373 1.259 13.229 6.496 939.069 1.495 28.893 3.137 0.44 235385. 0.2592
|
|
58.66 0.5704 0.7765 0.0477 0.0350 1.183 12.431 5.874 882.451 1.404 26.129 3.019 0.44 236037. 0.2372
|
|
61.60 0.5989 0.7829 0.0426 0.0326 1.100 11.550 5.241 819.917 1.305 23.311 2.899 0.44 236714. 0.2152
|
|
64.53 0.6275 0.7848 0.0373 0.0298 1.008 10.587 4.597 751.521 1.196 20.447 2.774 0.44 237417. 0.1928
|
|
67.46 0.6560 0.7812 0.0320 0.0269 0.908 9.542 3.944 677.349 1.078 17.545 2.641 0.44 238146. 0.1701
|
|
70.40 0.6845 0.7697 0.0267 0.0237 0.801 8.418 3.286 597.538 0.951 14.615 2.494 0.44 238901. 0.1466
|
|
73.33 0.7130 0.7466 0.0213 0.0203 0.687 7.217 2.623 512.291 0.815 11.667 2.322 0.44 239681. 0.1219
|
|
76.26 0.7415 0.7041 0.0159 0.0168 0.566 5.943 1.959 421.909 0.671 8.714 2.106 0.44 240488. 0.0956
|
|
79.19 0.7701 0.6250 0.0105 0.0130 0.438 4.604 1.297 326.801 0.520 5.770 1.800 0.44 241319. 0.0665
|
|
82.13 0.7986 0.4599 0.0052 0.0090 0.305 3.204 0.641 227.454 0.362 2.849 1.277 0.44 242172. 0.0331
|
|
85.06 0.8271 -0.0270 -0.0002 0.0049 0.164 1.725 -0.020 122.434 0.195 -0.087 -0.072 0.45 242960. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 7000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1112 0.0403 2.158 19.434 18.641 1609.468 2.196 82.915 5.253 0.50 265830. 0.7353
|
|
3.45 0.0287 0.0768 0.1101 0.0412 2.210 19.895 18.453 1647.675 2.248 82.080 5.080 0.50 266045. 0.7074
|
|
6.90 0.0575 0.1484 0.1088 0.0422 2.260 20.352 18.241 1685.506 2.299 81.135 4.909 0.50 266284. 0.6796
|
|
10.35 0.0862 0.2150 0.1074 0.0431 2.310 20.796 18.001 1722.253 2.349 80.069 4.741 0.50 266548. 0.6520
|
|
13.80 0.1150 0.2768 0.1058 0.0439 2.356 21.217 17.732 1757.191 2.397 78.870 4.577 0.50 266837. 0.6248
|
|
17.25 0.1437 0.3340 0.1040 0.0448 2.400 21.608 17.429 1789.526 2.441 77.526 4.418 0.50 267154. 0.5979
|
|
20.69 0.1725 0.3868 0.1020 0.0455 2.439 21.957 17.092 1818.411 2.481 76.026 4.263 0.50 267498. 0.5714
|
|
24.14 0.2012 0.4355 0.0997 0.0461 2.471 22.253 16.717 1842.945 2.514 74.356 4.114 0.50 267872. 0.5453
|
|
27.59 0.2300 0.4803 0.0973 0.0466 2.497 22.485 16.301 1862.156 2.540 72.505 3.970 0.50 268274. 0.5197
|
|
31.04 0.2587 0.5215 0.0945 0.0469 2.514 22.640 15.840 1874.965 2.558 70.458 3.832 0.50 268707. 0.4944
|
|
34.49 0.2875 0.5593 0.0915 0.0470 2.521 22.703 15.333 1880.190 2.565 68.199 3.699 0.50 269170. 0.4695
|
|
37.94 0.3162 0.5939 0.0882 0.0469 2.517 22.660 14.774 1876.646 2.560 65.717 3.571 0.51 269664. 0.4450
|
|
41.39 0.3450 0.6257 0.0845 0.0466 2.499 22.500 14.166 1863.419 2.542 63.011 3.448 0.51 270188. 0.4207
|
|
44.84 0.3737 0.6546 0.0806 0.0460 2.468 22.218 13.511 1840.023 2.510 60.095 3.330 0.51 270743. 0.3968
|
|
48.29 0.4024 0.6810 0.0764 0.0452 2.422 21.811 12.812 1806.329 2.464 56.989 3.217 0.51 271330. 0.3733
|
|
51.74 0.4312 0.7049 0.0721 0.0441 2.363 21.280 12.076 1762.400 2.404 53.716 3.108 0.51 271947. 0.3501
|
|
55.18 0.4599 0.7263 0.0675 0.0427 2.291 20.628 11.307 1708.354 2.331 50.295 3.002 0.51 272595. 0.3273
|
|
58.63 0.4887 0.7452 0.0627 0.0411 2.205 19.854 10.509 1644.309 2.243 46.746 2.899 0.51 273274. 0.3047
|
|
62.08 0.5174 0.7614 0.0578 0.0393 2.106 18.961 9.686 1570.358 2.142 43.085 2.798 0.51 273983. 0.2823
|
|
65.53 0.5462 0.7749 0.0528 0.0372 1.994 17.950 8.841 1486.568 2.028 39.324 2.697 0.51 274724. 0.2600
|
|
68.98 0.5749 0.7854 0.0476 0.0348 1.868 16.820 7.976 1392.996 1.900 35.478 2.597 0.51 275495. 0.2378
|
|
72.43 0.6037 0.7922 0.0423 0.0323 1.730 15.573 7.094 1289.711 1.759 31.556 2.495 0.51 276297. 0.2154
|
|
75.88 0.6324 0.7947 0.0370 0.0294 1.578 14.210 6.199 1176.810 1.605 27.571 2.389 0.51 277129. 0.1928
|
|
79.33 0.6612 0.7915 0.0316 0.0264 1.414 12.732 5.291 1054.446 1.438 23.534 2.276 0.51 277993. 0.1697
|
|
82.78 0.6899 0.7803 0.0261 0.0231 1.238 11.143 4.375 922.859 1.259 19.459 2.150 0.51 278886. 0.1458
|
|
86.23 0.7187 0.7568 0.0206 0.0196 1.049 9.447 3.453 782.411 1.067 15.361 2.002 0.52 279811. 0.1206
|
|
89.67 0.7474 0.7122 0.0151 0.0158 0.850 7.651 2.531 633.634 0.864 11.257 1.812 0.52 280765. 0.0934
|
|
93.12 0.7762 0.6254 0.0096 0.0119 0.640 5.763 1.612 477.244 0.651 7.169 1.532 0.52 281748. 0.0630
|
|
96.57 0.8049 0.4285 0.0042 0.0079 0.421 3.792 0.701 314.026 0.428 3.117 1.012 0.52 282755. 0.0275
|
|
100.02 0.8336
|
|
|
|
|
|
|
|
PROP RPM = 8000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1122 0.0405 3.243 25.550 24.557 2418.282 2.887 109.228 4.606 0.57 303781. 0.7399
|
|
3.93 0.0287 0.0767 0.1111 0.0415 3.322 26.170 24.323 2476.963 2.957 108.187 4.454 0.57 304026. 0.7121
|
|
7.86 0.0573 0.1483 0.1099 0.0425 3.400 26.785 24.056 2535.160 3.026 107.003 4.304 0.57 304297. 0.6843
|
|
11.79 0.0860 0.2148 0.1085 0.0434 3.476 27.383 23.754 2591.803 3.094 105.659 4.157 0.57 304597. 0.6568
|
|
15.72 0.1146 0.2766 0.1070 0.0443 3.548 27.953 23.413 2645.756 3.158 104.140 4.014 0.57 304927. 0.6296
|
|
19.65 0.1433 0.3337 0.1052 0.0452 3.615 28.482 23.028 2695.794 3.218 102.428 3.874 0.57 305288. 0.6027
|
|
23.58 0.1719 0.3865 0.1032 0.0459 3.675 28.955 22.596 2740.617 3.271 100.507 3.740 0.58 305680. 0.5763
|
|
27.51 0.2006 0.4352 0.1010 0.0466 3.726 29.359 22.114 2778.848 3.317 98.362 3.609 0.58 306106. 0.5502
|
|
31.43 0.2292 0.4801 0.0986 0.0471 3.767 29.678 21.577 2809.012 3.353 95.974 3.484 0.58 306564. 0.5246
|
|
35.36 0.2579 0.5214 0.0958 0.0474 3.794 29.894 20.981 2829.497 3.377 93.325 3.363 0.58 307058. 0.4994
|
|
39.29 0.2866 0.5594 0.0928 0.0476 3.807 29.990 20.323 2838.520 3.388 90.395 3.247 0.58 307585. 0.4746
|
|
43.22 0.3152 0.5942 0.0895 0.0475 3.801 29.945 19.597 2834.292 3.383 87.167 3.136 0.58 308148. 0.4501
|
|
47.15 0.3439 0.6262 0.0859 0.0472 3.775 29.745 18.804 2815.386 3.361 83.641 3.029 0.58 308746. 0.4259
|
|
51.08 0.3725 0.6555 0.0820 0.0466 3.729 29.382 17.948 2781.014 3.320 79.831 2.927 0.58 309379. 0.4020
|
|
55.01 0.4012 0.6822 0.0778 0.0458 3.662 28.853 17.033 2730.956 3.260 75.764 2.829 0.58 310047. 0.3785
|
|
58.94 0.4298 0.7065 0.0734 0.0447 3.574 28.160 16.068 2665.305 3.181 71.470 2.734 0.58 310750. 0.3553
|
|
62.87 0.4585 0.7284 0.0688 0.0433 3.466 27.303 15.058 2584.257 3.085 66.977 2.643 0.58 311488. 0.3325
|
|
66.80 0.4871 0.7479 0.0640 0.0417 3.336 26.287 14.009 2488.008 2.970 62.311 2.554 0.58 312261. 0.3099
|
|
70.73 0.5158 0.7648 0.0590 0.0398 3.187 25.111 12.926 2376.720 2.837 57.493 2.467 0.58 313069. 0.2875
|
|
74.66 0.5445 0.7792 0.0540 0.0377 3.018 23.777 11.812 2250.508 2.686 52.541 2.381 0.58 313911. 0.2652
|
|
78.59 0.5731 0.7906 0.0488 0.0353 2.829 22.287 10.673 2109.470 2.518 47.471 2.295 0.58 314789. 0.2430
|
|
82.52 0.6018 0.7987 0.0434 0.0327 2.620 20.642 9.510 1953.709 2.332 42.300 2.208 0.58 315701. 0.2207
|
|
86.44 0.6304 0.8027 0.0380 0.0299 2.392 18.842 8.328 1783.368 2.129 37.042 2.118 0.59 316648. 0.1981
|
|
90.37 0.6591 0.8014 0.0326 0.0268 2.144 16.890 7.130 1598.671 1.908 31.712 2.023 0.59 317630. 0.1751
|
|
94.30 0.6877 0.7928 0.0270 0.0235 1.877 14.791 5.919 1399.967 1.671 26.328 1.918 0.59 318647. 0.1513
|
|
98.23 0.7164 0.7731 0.0215 0.0199 1.593 12.549 4.701 1187.785 1.418 20.910 1.795 0.59 319697. 0.1262
|
|
102.16 0.7450 0.7342 0.0159 0.0161 1.291 10.173 3.480 962.898 1.149 15.480 1.639 0.59 320782. 0.0991
|
|
106.09 0.7737 0.6573 0.0103 0.0122 0.974 7.674 2.263 726.371 0.867 10.067 1.413 0.59 321900. 0.0689
|
|
110.02 0.8024 0.4819 0.0048 0.0080 0.643 5.065 1.056 479.419 0.572 4.697 0.999 0.59 323047. 0.0333
|
|
113.95 0.8310
|
|
|
|
|
|
|
|
PROP RPM = 9000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1133 0.0410 4.670 32.702 31.382 3482.118 3.695 139.586 4.088 0.65 341720. 0.7423
|
|
4.41 0.0286 0.0764 0.1123 0.0420 4.785 33.508 31.104 3567.937 3.786 138.351 3.954 0.65 341994. 0.7149
|
|
8.81 0.0571 0.1476 0.1111 0.0430 4.899 34.310 30.786 3653.343 3.876 136.935 3.822 0.65 342298. 0.6875
|
|
13.22 0.0857 0.2139 0.1098 0.0440 5.011 35.093 30.422 3736.743 3.965 135.316 3.693 0.65 342633. 0.6603
|
|
17.62 0.1142 0.2755 0.1083 0.0449 5.118 35.842 30.007 3816.459 4.049 133.470 3.566 0.65 343003. 0.6333
|
|
22.03 0.1428 0.3325 0.1066 0.0458 5.217 36.539 29.536 3890.674 4.128 131.377 3.443 0.65 343407. 0.6066
|
|
26.43 0.1713 0.3852 0.1047 0.0466 5.307 37.166 29.005 3957.429 4.199 129.012 3.324 0.65 343847. 0.5804
|
|
30.84 0.1999 0.4339 0.1025 0.0472 5.384 37.703 28.407 4014.678 4.260 126.355 3.209 0.65 344324. 0.5545
|
|
35.24 0.2285 0.4788 0.1001 0.0478 5.445 38.131 27.739 4060.240 4.308 123.384 3.099 0.65 344839. 0.5291
|
|
39.65 0.2570 0.5201 0.0974 0.0481 5.487 38.427 26.995 4091.766 4.341 120.074 2.992 0.65 345392. 0.5040
|
|
44.05 0.2856 0.5582 0.0945 0.0483 5.507 38.568 26.169 4106.698 4.357 116.399 2.890 0.65 345984. 0.4793
|
|
48.46 0.3141 0.5932 0.0912 0.0483 5.501 38.528 25.256 4102.444 4.353 112.338 2.792 0.65 346615. 0.4549
|
|
52.86 0.3427 0.6254 0.0875 0.0480 5.467 38.287 24.255 4076.873 4.326 107.886 2.698 0.65 347286. 0.4308
|
|
57.27 0.3712 0.6549 0.0836 0.0474 5.403 37.836 23.171 4028.765 4.275 103.062 2.609 0.65 347996. 0.4071
|
|
61.67 0.3998 0.6820 0.0794 0.0466 5.307 37.169 22.010 3957.756 4.199 97.900 2.522 0.65 348745. 0.3836
|
|
66.08 0.4284 0.7067 0.0750 0.0455 5.182 36.288 20.782 3863.981 4.100 92.438 2.439 0.65 349534. 0.3605
|
|
70.48 0.4569 0.7290 0.0704 0.0441 5.026 35.197 19.495 3747.750 3.976 86.713 2.359 0.65 350361. 0.3377
|
|
74.89 0.4855 0.7491 0.0655 0.0425 4.840 33.897 18.156 3609.396 3.830 80.758 2.282 0.65 351228. 0.3152
|
|
79.29 0.5140 0.7667 0.0605 0.0406 4.625 32.393 16.772 3449.184 3.660 74.602 2.206 0.65 352133. 0.2928
|
|
83.70 0.5426 0.7818 0.0554 0.0384 4.382 30.685 15.348 3267.314 3.467 68.269 2.131 0.66 353077. 0.2706
|
|
88.11 0.5711 0.7942 0.0501 0.0361 4.109 28.775 13.890 3063.945 3.251 61.781 2.056 0.66 354060. 0.2484
|
|
92.51 0.5997 0.8034 0.0448 0.0334 3.807 26.664 12.401 2839.236 3.013 55.158 1.981 0.66 355081. 0.2261
|
|
96.92 0.6283 0.8089 0.0393 0.0305 3.478 24.356 10.885 2593.389 2.752 48.418 1.904 0.66 356142. 0.2036
|
|
101.32 0.6568 0.8095 0.0337 0.0274 3.120 21.851 9.348 2326.721 2.469 41.581 1.822 0.66 357241. 0.1806
|
|
105.73 0.6854 0.8033 0.0281 0.0240 2.735 19.156 7.794 2039.706 2.164 34.669 1.733 0.66 358378. 0.1569
|
|
110.13 0.7139 0.7871 0.0225 0.0204 2.324 16.276 6.229 1733.082 1.839 27.707 1.630 0.66 359554. 0.1319
|
|
114.54 0.7425 0.7537 0.0168 0.0166 1.888 13.222 4.659 1407.926 1.494 20.723 1.501 0.66 360768. 0.1050
|
|
118.94 0.7710 0.6862 0.0112 0.0125 1.429 10.009 3.092 1065.734 1.131 13.755 1.316 0.67 362018. 0.0750
|
|
123.35 0.7996 0.5322 0.0055 0.0083 0.950 6.652 1.537 708.313 0.752 6.836 0.984 0.67 363302. 0.0396
|
|
127.75 0.8282 -0.0289 -0.0001 0.0039 0.440 3.083 -0.037 328.301 0.348 -0.166 -0.052 0.67 364432. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 10000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1145 0.0422 6.591 41.543 39.154 4915.042 4.694 174.155 3.613 0.72 379647. 0.7329
|
|
4.90 0.0286 0.0752 0.1136 0.0432 6.748 42.530 38.840 5031.758 4.805 172.759 3.501 0.72 379950. 0.7073
|
|
9.80 0.0572 0.1456 0.1125 0.0442 6.903 43.511 38.475 5147.866 4.916 171.138 3.390 0.72 380286. 0.6817
|
|
14.70 0.0857 0.2114 0.1113 0.0451 7.055 44.469 38.054 5261.179 5.024 169.264 3.281 0.72 380659. 0.6561
|
|
19.59 0.1143 0.2726 0.1098 0.0461 7.200 45.384 37.569 5369.407 5.127 167.105 3.174 0.72 381069. 0.6306
|
|
24.49 0.1429 0.3295 0.1082 0.0469 7.335 46.234 37.012 5470.057 5.224 164.628 3.069 0.72 381518. 0.6053
|
|
29.39 0.1715 0.3823 0.1064 0.0477 7.457 46.999 36.377 5560.492 5.310 161.804 2.967 0.72 382008. 0.5802
|
|
34.29 0.2001 0.4312 0.1042 0.0484 7.561 47.653 35.657 5637.904 5.384 158.603 2.869 0.72 382540. 0.5553
|
|
39.19 0.2286 0.4764 0.1019 0.0489 7.643 48.172 34.846 5699.355 5.442 154.994 2.773 0.72 383114. 0.5307
|
|
44.09 0.2572 0.5181 0.0992 0.0493 7.700 48.530 33.936 5741.620 5.483 150.947 2.681 0.72 383732. 0.5063
|
|
48.99 0.2858 0.5566 0.0962 0.0494 7.726 48.695 32.920 5761.156 5.501 146.429 2.592 0.72 384393. 0.4821
|
|
53.88 0.3144 0.5920 0.0929 0.0494 7.717 48.636 31.792 5754.261 5.495 141.411 2.506 0.72 385098. 0.4581
|
|
58.78 0.3430 0.6245 0.0893 0.0490 7.668 48.328 30.550 5717.805 5.460 135.888 2.423 0.72 385847. 0.4342
|
|
63.68 0.3715 0.6544 0.0854 0.0485 7.577 47.754 29.200 5649.863 5.395 129.881 2.344 0.72 386639. 0.4106
|
|
68.58 0.4001 0.6819 0.0811 0.0476 7.442 46.908 27.750 5549.721 5.300 123.433 2.268 0.72 387476. 0.3873
|
|
73.48 0.4287 0.7070 0.0766 0.0465 7.265 45.789 26.213 5417.401 5.173 116.594 2.195 0.72 388356. 0.3643
|
|
78.38 0.4573 0.7298 0.0719 0.0451 7.045 44.402 24.598 5253.244 5.016 109.412 2.124 0.73 389280. 0.3415
|
|
83.28 0.4859 0.7503 0.0670 0.0434 6.782 42.749 22.916 5057.672 4.830 101.931 2.055 0.73 390246. 0.3189
|
|
88.17 0.5144 0.7685 0.0619 0.0414 6.479 40.834 21.175 4831.128 4.613 94.188 1.988 0.73 391256. 0.2966
|
|
93.07 0.5430 0.7843 0.0567 0.0392 6.134 38.660 19.383 4573.942 4.368 86.215 1.922 0.73 392309. 0.2743
|
|
97.97 0.5716 0.7974 0.0513 0.0368 5.748 36.229 17.545 4286.371 4.093 78.039 1.857 0.73 393405. 0.2521
|
|
102.87 0.6002 0.8075 0.0458 0.0340 5.322 33.544 15.667 3968.657 3.790 69.687 1.791 0.73 394544. 0.2298
|
|
107.77 0.6288 0.8140 0.0402 0.0311 4.856 30.606 13.755 3621.088 3.458 61.182 1.723 0.73 395726. 0.2071
|
|
112.67 0.6573 0.8158 0.0345 0.0278 4.350 27.420 11.814 3244.117 3.098 52.548 1.652 0.73 396950. 0.1840
|
|
117.57 0.6859 0.8112 0.0288 0.0243 3.807 23.992 9.850 2838.521 2.711 43.814 1.574 0.73 398218. 0.1601
|
|
122.47 0.7145 0.7968 0.0230 0.0206 3.226 20.332 7.871 2405.512 2.297 35.011 1.484 0.74 399527. 0.1350
|
|
127.36 0.7431 0.7655 0.0172 0.0167 2.611 16.456 5.885 1946.897 1.859 26.175 1.371 0.74 400879. 0.1078
|
|
132.26 0.7717 0.7002 0.0114 0.0126 1.965 12.385 3.901 1465.248 1.399 17.351 1.208 0.74 402271. 0.0773
|
|
137.16 0.8002 0.5462 0.0056 0.0083 1.292 8.146 1.930 963.749 0.920 8.585 0.908 0.74 403700. 0.0409
|
|
142.06 0.8288 -0.0532 -0.0002 0.0037 0.575 3.624 -0.081 428.767 0.409 -0.359 -0.085 0.74 404880. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 11000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1157 0.0455 9.469 54.257 47.884 7061.143 6.130 212.990 3.076 0.79 417560. 0.6900
|
|
5.39 0.0286 0.0707 0.1149 0.0465 9.667 55.391 47.550 7208.731 6.258 211.503 2.992 0.79 417890. 0.6688
|
|
10.78 0.0572 0.1375 0.1139 0.0474 9.862 56.505 47.157 7353.766 6.384 209.754 2.909 0.79 418258. 0.6475
|
|
16.17 0.0858 0.2004 0.1128 0.0483 10.048 57.575 46.695 7492.978 6.505 207.700 2.827 0.79 418665. 0.6262
|
|
21.56 0.1144 0.2596 0.1115 0.0491 10.223 58.575 46.155 7623.095 6.618 205.297 2.746 0.79 419115. 0.6048
|
|
26.95 0.1430 0.3152 0.1100 0.0499 10.381 59.479 45.526 7740.740 6.720 202.500 2.668 0.79 419609. 0.5835
|
|
32.34 0.1715 0.3674 0.1082 0.0505 10.517 60.261 44.799 7842.517 6.808 199.267 2.591 0.79 420148. 0.5622
|
|
37.73 0.2001 0.4162 0.1062 0.0511 10.628 60.894 43.964 7924.953 6.880 195.554 2.516 0.79 420734. 0.5409
|
|
43.12 0.2287 0.4619 0.1039 0.0515 10.707 61.352 43.013 7984.521 6.932 191.322 2.443 0.79 421368. 0.5195
|
|
48.51 0.2573 0.5046 0.1013 0.0517 10.752 61.605 41.936 8017.491 6.960 186.530 2.372 0.79 422050. 0.4980
|
|
53.91 0.2859 0.5443 0.0984 0.0517 10.755 61.622 40.722 8019.721 6.962 181.133 2.303 0.79 422780. 0.4765
|
|
59.30 0.3145 0.5811 0.0951 0.0515 10.711 61.370 39.365 7986.909 6.934 175.097 2.236 0.79 423559. 0.4547
|
|
64.69 0.3431 0.6153 0.0915 0.0510 10.615 60.820 37.862 7915.317 6.871 168.410 2.170 0.79 424387. 0.4328
|
|
70.08 0.3717 0.6468 0.0875 0.0503 10.464 59.955 36.218 7802.720 6.774 161.099 2.105 0.80 425263. 0.4108
|
|
75.47 0.4003 0.6758 0.0832 0.0493 10.257 58.770 34.446 7648.447 6.640 153.217 2.043 0.80 426188. 0.3887
|
|
80.86 0.4289 0.7024 0.0787 0.0480 9.994 57.265 32.560 7452.659 6.470 144.828 1.982 0.80 427161. 0.3666
|
|
86.25 0.4575 0.7267 0.0739 0.0465 9.677 55.445 30.574 7215.779 6.264 135.992 1.922 0.80 428182. 0.3445
|
|
91.64 0.4860 0.7485 0.0689 0.0447 9.304 53.312 28.500 6938.237 6.023 126.767 1.863 0.80 429250. 0.3224
|
|
97.03 0.5146 0.7679 0.0637 0.0427 8.878 50.870 26.349 6620.308 5.747 117.200 1.805 0.80 430365. 0.3004
|
|
102.42 0.5432 0.7848 0.0583 0.0404 8.398 48.117 24.131 6262.090 5.436 107.334 1.748 0.80 431528. 0.2783
|
|
107.81 0.5718 0.7990 0.0528 0.0378 7.863 45.055 21.854 5863.632 5.090 97.206 1.690 0.80 432738. 0.2562
|
|
113.20 0.6004 0.8100 0.0472 0.0350 7.276 41.689 19.525 5425.584 4.710 86.846 1.632 0.80 433994. 0.2338
|
|
118.59 0.6290 0.8173 0.0414 0.0319 6.636 38.021 17.151 4948.141 4.296 76.286 1.572 0.81 435298. 0.2111
|
|
123.98 0.6576 0.8198 0.0356 0.0286 5.944 34.056 14.738 4432.091 3.848 65.555 1.508 0.81 436648. 0.1877
|
|
129.37 0.6862 0.8153 0.0297 0.0250 5.202 29.808 12.295 3879.321 3.368 54.688 1.438 0.81 438046. 0.1634
|
|
134.76 0.7148 0.7999 0.0238 0.0212 4.416 25.301 9.829 3292.772 2.859 43.721 1.354 0.81 439489. 0.1376
|
|
140.15 0.7434 0.7655 0.0178 0.0172 3.589 20.565 7.352 2676.398 2.323 32.701 1.246 0.81 440978. 0.1095
|
|
145.54 0.7720 0.6930 0.0118 0.0131 2.730 15.640 4.874 2035.485 1.767 21.679 1.086 0.81 442512. 0.0777
|
|
150.94 0.8005 0.5252 0.0058 0.0089 1.846 10.575 2.408 1376.281 1.195 10.713 0.794 0.81 444086. 0.0399
|
|
156.33 0.8291 -0.0484 -0.0003 0.0044 0.914 5.236 -0.106 681.450 0.592 -0.472 -0.071 0.82 445401. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1166 0.0525 14.194 74.555 57.435 10584.831 8.423 255.469 2.461 0.86 455466. 0.6047
|
|
5.95 0.0289 0.0627 0.1159 0.0535 14.447 75.879 57.100 10772.882 8.573 253.980 2.404 0.86 455825. 0.5889
|
|
11.90 0.0579 0.1225 0.1151 0.0544 14.690 77.158 56.700 10954.392 8.717 252.202 2.348 0.86 456226. 0.5731
|
|
17.85 0.0868 0.1794 0.1141 0.0552 14.917 78.347 56.222 11123.297 8.852 250.075 2.293 0.86 456673. 0.5573
|
|
23.80 0.1157 0.2336 0.1130 0.0560 15.118 79.405 55.651 11273.408 8.971 247.533 2.239 0.86 457167. 0.5415
|
|
29.75 0.1446 0.2853 0.1116 0.0566 15.286 80.286 54.971 11398.538 9.071 244.510 2.187 0.86 457711. 0.5257
|
|
35.70 0.1736 0.3346 0.1100 0.0571 15.411 80.946 54.167 11492.294 9.145 240.935 2.138 0.86 458307. 0.5101
|
|
41.65 0.2025 0.3816 0.1081 0.0573 15.489 81.354 53.226 11550.226 9.191 236.748 2.090 0.86 458957. 0.4943
|
|
47.60 0.2314 0.4265 0.1058 0.0574 15.513 81.482 52.134 11568.389 9.206 231.891 2.044 0.86 459661. 0.4784
|
|
53.54 0.2603 0.4693 0.1033 0.0573 15.479 81.304 50.878 11543.024 9.186 226.305 1.999 0.86 460421. 0.4623
|
|
59.49 0.2893 0.5100 0.1004 0.0569 15.382 80.791 49.446 11470.272 9.128 219.934 1.955 0.87 461235. 0.4457
|
|
65.44 0.3182 0.5485 0.0971 0.0563 15.215 79.917 47.826 11346.089 9.029 212.728 1.912 0.87 462105. 0.4286
|
|
71.39 0.3471 0.5849 0.0934 0.0554 14.975 78.656 46.014 11167.114 8.887 204.671 1.869 0.87 463031. 0.4110
|
|
77.34 0.3760 0.6193 0.0894 0.0543 14.660 77.000 44.019 10931.980 8.699 195.794 1.826 0.87 464011. 0.3928
|
|
83.29 0.4050 0.6514 0.0850 0.0528 14.271 74.955 41.854 10641.635 8.468 186.168 1.784 0.87 465045. 0.3741
|
|
89.24 0.4339 0.6813 0.0803 0.0511 13.810 72.536 39.541 10298.262 8.195 175.878 1.742 0.87 466133. 0.3550
|
|
95.19 0.4628 0.7090 0.0753 0.0492 13.282 69.760 37.097 9904.076 7.881 165.007 1.699 0.87 467275. 0.3354
|
|
101.14 0.4917 0.7342 0.0701 0.0470 12.687 66.636 34.539 9460.588 7.528 153.627 1.656 0.87 468469. 0.3155
|
|
107.09 0.5207 0.7569 0.0647 0.0445 12.027 63.172 31.880 8968.730 7.137 141.804 1.612 0.87 469716. 0.2951
|
|
113.04 0.5496 0.7770 0.0592 0.0418 11.303 59.366 29.134 8428.481 6.707 129.589 1.568 0.87 471016. 0.2743
|
|
118.99 0.5785 0.7941 0.0534 0.0389 10.513 55.218 26.310 7839.503 6.238 117.029 1.522 0.88 472368. 0.2531
|
|
124.94 0.6074 0.8072 0.0475 0.0358 9.666 50.767 23.418 7207.668 5.736 104.162 1.474 0.88 473772. 0.2312
|
|
130.89 0.6364 0.8144 0.0415 0.0325 8.770 46.066 20.464 6540.120 5.204 91.026 1.419 0.88 475228. 0.2081
|
|
136.84 0.6653 0.8118 0.0354 0.0290 7.847 41.215 17.457 5851.479 4.656 77.650 1.353 0.88 476735. 0.1833
|
|
142.79 0.6942 0.7980 0.0293 0.0254 6.875 36.109 14.410 5126.598 4.080 64.094 1.275 0.88 478294. 0.1569
|
|
148.74 0.7231 0.7667 0.0230 0.0217 5.863 30.794 11.333 4371.999 3.479 50.410 1.176 0.88 479905. 0.1283
|
|
154.68 0.7521 0.7049 0.0167 0.0179 4.823 25.334 8.243 3596.804 2.862 36.663 1.039 0.89 481566. 0.0967
|
|
160.63 0.7810 0.5857 0.0105 0.0140 3.770 19.802 5.156 2811.385 2.237 22.932 0.832 0.89 483276. 0.0612
|
|
166.58 0.8099 0.3416 0.0042 0.0101 2.717 14.271 2.089 2026.048 1.612 9.294 0.468 0.89 485025. 0.0219
|
|
172.53 0.8388
|
|
|
|
|
|
|
|
PROP RPM = 13000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1151 0.0600 20.602 99.888 66.525 15363.271 11.285 295.902 1.964 0.93 493482. 0.5193
|
|
6.49 0.0291 0.0548 0.1145 0.0609 20.914 101.396 66.198 15595.241 11.456 294.450 1.925 0.93 493867. 0.5078
|
|
12.98 0.0582 0.1073 0.1139 0.0618 21.221 102.887 65.812 15824.596 11.624 292.730 1.886 0.93 494297. 0.4961
|
|
19.47 0.0874 0.1577 0.1131 0.0626 21.516 104.316 65.350 16044.415 11.786 290.677 1.847 0.93 494775. 0.4841
|
|
25.96 0.1165 0.2058 0.1121 0.0634 21.788 105.634 64.798 16247.071 11.934 288.222 1.809 0.93 495305. 0.4721
|
|
32.45 0.1456 0.2519 0.1110 0.0641 22.025 106.785 64.138 16424.113 12.065 285.285 1.771 0.93 495889. 0.4599
|
|
38.93 0.1747 0.2960 0.1096 0.0647 22.216 107.711 63.351 16566.576 12.169 281.784 1.734 0.93 496529. 0.4475
|
|
45.42 0.2039 0.3383 0.1080 0.0651 22.348 108.352 62.417 16665.139 12.242 277.629 1.699 0.94 497228. 0.4351
|
|
51.91 0.2330 0.3788 0.1061 0.0652 22.409 108.645 61.315 16710.141 12.275 272.730 1.664 0.94 497987. 0.4225
|
|
58.40 0.2621 0.4176 0.1038 0.0652 22.383 108.523 60.024 16691.371 12.261 266.988 1.631 0.94 498808. 0.4097
|
|
64.89 0.2912 0.4549 0.1012 0.0648 22.258 107.914 58.520 16597.807 12.192 260.298 1.599 0.94 499690. 0.3966
|
|
71.38 0.3203 0.4909 0.0982 0.0641 22.016 106.741 56.780 16417.268 12.059 252.556 1.569 0.94 500636. 0.3832
|
|
77.87 0.3495 0.5256 0.0948 0.0630 21.646 104.947 54.791 16141.458 11.857 243.708 1.540 0.94 501644. 0.3694
|
|
84.36 0.3786 0.5591 0.0909 0.0616 21.144 102.515 52.556 15767.334 11.582 233.769 1.512 0.94 502715. 0.3553
|
|
90.85 0.4077 0.5915 0.0867 0.0597 20.514 99.460 50.091 15297.409 11.237 222.807 1.485 0.94 503848. 0.3408
|
|
97.34 0.4368 0.6227 0.0820 0.0575 19.764 95.824 47.419 14738.172 10.826 210.920 1.459 0.94 505041. 0.3258
|
|
103.82 0.4660 0.6526 0.0771 0.0550 18.906 91.662 44.563 14098.050 10.356 198.216 1.434 0.94 506295. 0.3103
|
|
110.31 0.4951 0.6808 0.0719 0.0523 17.950 87.027 41.546 13385.199 9.832 184.796 1.408 0.94 507609. 0.2942
|
|
116.80 0.5242 0.7073 0.0664 0.0492 16.905 81.960 38.387 12605.932 9.260 170.747 1.381 0.95 508980. 0.2774
|
|
123.29 0.5533 0.7315 0.0607 0.0459 15.776 76.487 35.104 11764.166 8.642 156.141 1.353 0.95 510410. 0.2600
|
|
129.78 0.5824 0.7533 0.0549 0.0424 14.568 70.631 31.711 10863.442 7.980 141.049 1.324 0.95 511898. 0.2417
|
|
136.27 0.6116 0.7719 0.0488 0.0387 13.286 64.413 28.224 9907.085 7.277 125.539 1.292 0.95 513442. 0.2225
|
|
142.76 0.6407 0.7835 0.0426 0.0349 11.977 58.070 24.652 8931.511 6.561 109.653 1.252 0.95 515044. 0.2015
|
|
149.25 0.6698 0.7750 0.0363 0.0314 10.778 52.255 20.989 8037.041 5.904 93.360 1.185 0.95 516701. 0.1759
|
|
155.74 0.6989 0.7429 0.0299 0.0281 9.647 46.773 17.259 7193.929 5.284 76.768 1.088 0.96 518414. 0.1465
|
|
162.23 0.7281 0.6860 0.0233 0.0248 8.510 41.261 13.497 6346.150 4.662 60.033 0.965 0.96 520184. 0.1149
|
|
168.72 0.7572 0.5929 0.0168 0.0215 7.384 35.798 9.731 5505.999 4.044 43.283 0.802 0.96 522008. 0.0811
|
|
175.20 0.7863 0.4459 0.0104 0.0183 6.285 30.471 5.998 4686.656 3.443 26.680 0.580 0.96 523886. 0.0461
|
|
181.69 0.8154 0.2166 0.0040 0.0152 5.224 25.328 2.335 3895.521 2.861 10.388 0.272 0.96 525811. 0.0135
|
|
188.18 0.8445
|
|
|
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